CA2575625C - An electricity transport conductor for overhead lines - Google Patents
An electricity transport conductor for overhead lines Download PDFInfo
- Publication number
- CA2575625C CA2575625C CA 2575625 CA2575625A CA2575625C CA 2575625 C CA2575625 C CA 2575625C CA 2575625 CA2575625 CA 2575625 CA 2575625 A CA2575625 A CA 2575625A CA 2575625 C CA2575625 C CA 2575625C
- Authority
- CA
- Canada
- Prior art keywords
- conductor
- core
- insulating material
- electricity transport
- wires
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 239000004020 conductor Substances 0.000 title claims abstract description 49
- 230000005611 electricity Effects 0.000 title claims abstract description 15
- 239000011810 insulating material Substances 0.000 claims abstract description 27
- 239000002131 composite material Substances 0.000 claims abstract description 14
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 13
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 13
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 12
- 239000000835 fiber Substances 0.000 claims abstract description 9
- 239000003822 epoxy resin Substances 0.000 claims abstract description 8
- 229920000647 polyepoxide Polymers 0.000 claims abstract description 8
- 239000011159 matrix material Substances 0.000 claims abstract description 6
- 239000004696 Poly ether ether ketone Substances 0.000 claims description 3
- 229920002530 polyetherether ketone Polymers 0.000 claims description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 2
- 229910052799 carbon Inorganic materials 0.000 claims description 2
- -1 poly (oxy-1,4-phenylene-oxy-1,4-phenylene-carbonyl-1,4-phenylene) Polymers 0.000 claims description 2
- 238000010438 heat treatment Methods 0.000 abstract description 5
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 239000010410 layer Substances 0.000 description 26
- 230000035882 stress Effects 0.000 description 7
- 229920001721 polyimide Polymers 0.000 description 6
- 229920000049 Carbon (fiber) Polymers 0.000 description 5
- 239000004917 carbon fiber Substances 0.000 description 5
- 239000004642 Polyimide Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- 239000003365 glass fiber Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 229920001187 thermosetting polymer Polymers 0.000 description 2
- 229920004695 VICTREX™ PEEK Polymers 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 239000012784 inorganic fiber Substances 0.000 description 1
- 229920001084 poly(chloroprene) Polymers 0.000 description 1
- 239000009719 polyimide resin Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 229920003002 synthetic resin Polymers 0.000 description 1
- 239000000057 synthetic resin Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B9/00—Power cables
- H01B9/008—Power cables for overhead application
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B1/00—Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
- H01B1/02—Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors mainly consisting of metals or alloys
- H01B1/023—Alloys based on aluminium
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B13/00—Apparatus or processes specially adapted for manufacturing conductors or cables
- H01B13/06—Insulating conductors or cables
- H01B13/14—Insulating conductors or cables by extrusion
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B5/00—Non-insulated conductors or conductive bodies characterised by their form
- H01B5/08—Several wires or the like stranded in the form of a rope
- H01B5/10—Several wires or the like stranded in the form of a rope stranded around a space, insulating material, or dissimilar conducting material
- H01B5/102—Several wires or the like stranded in the form of a rope stranded around a space, insulating material, or dissimilar conducting material stranded around a high tensile strength core
- H01B5/105—Several wires or the like stranded in the form of a rope stranded around a space, insulating material, or dissimilar conducting material stranded around a high tensile strength core composed of synthetic filaments, e.g. glass-fibres
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
- H01B9/00—Power cables
- H01B9/006—Constructional features relating to the conductors
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Non-Insulated Conductors (AREA)
- Insulating Bodies (AREA)
- Insulated Conductors (AREA)
Abstract
The invention relates to a method of fabricating an electricity transport conductor, in particular for overhead power lines, that are to operate at an operating temperature greater than or equal to 200°C, and comprising at least one composite central core 1 made of continuous fibers impregnated with an epoxy resin matrix, the core being covered in at least one layer of insulating material 2, and conductor wires 3 of aluminum or aluminum alloy being wound around the core. According to the invention, said insulating material is compatible with said operating temperature and is put into place on said core 1 without subsequent heating.
Description
AN ELECTRICITY TRANSPORT CONDUCTOR FOR OVERHEAD LINES
The invention relates to an electricity transport conductor for high voltage overhead lines.
The invention ,relates more particularly to a conductor comprising at least one composite central core made up of continuous fibers and impregnated by a matrix of thermosetting resin, and conductor wires of aluminum or aluminum alloy disposed around the core.
Such a conductor is described in patent document JP 03-129606.
In that prior art document, the composite core is constituted by organic or inorganic fibers, e.g. aramid, silicon carbide, or carbon fibers, impregnated by a synthetic resin, preferably an epoxy resin. That core may be coated in a polyimide resin or it may be taped in a polyimide film, forming an insulating layer. Conductor wires of aluminum are wound around such a core or a set of such cores in order to form an electricity transport conductor.
The function of the polyimide covering is to avoid problems of corrosion at the interface between the conductor wires and the core including carbon fibers.
Regardless of whether the polyimide covering is made by coating or by taping, it is necessary to pass the covered core through a drying oven after the covering has been put into place.
With conductors for overhead lines, there are three types of temperature to be taken into consideration:
= the maximum temperature acceptable under steady conditions;
= the maximum temperature acceptable during overloads of short, medium, or long duration; and = the maximum temperature acceptable during a short circuit.
It can be desired to make overhead line conductors that are designed in such a manner that the maximum acceptable temperature in all three of the above circumstances is greater than or equal to 200 C, which temperature is referred to below as the operating temperature.
In order to form a continuous insulating sheath of polyimide around the core, it is necessary to heat said taped or coated polyimide layer to a temperature greater than 300 C. Under such conditions, the insulating layer as formed in that way is compatible with a conductor having its operating temperature greater than or equal to 200 C.
Unfortunately, applying heat treatment at such a temperature greater than 300 C degrades the epoxy resin of the core, which begins to deteriorate at a temperature of about 250 C.
It can therefore be seen that fabrication in that way does not enable an electric cable to be obtained having an operating temperature that can be as high as 200 C or more.
According to the present invention, there is provided an electricity transport conductor, having an operating temperature greater than or equal to 200 C, said conductor comprising a plurality of composite central cores made of continuous fibers impregnated by a matrix of epoxy resin, wherein conductor wires of aluminum or aluminum alloy being wound directly around the composite central cores to form at least one layer covering said composite central cores and characterized in that each of said cores is covered in at least one extruded layer of insulating material.
Preferably, there is also provided a method of fabricating an electricity transport conductor, in particular for overhead power lines, having an operating temperature greater than or equal to 200 C and including at least one composite central core made of continuous fibers impregnated by a matrix of epoxy resin, the core being covered in at least one layer of insulating material, and conductor wires of aluminum or aluminum alloy being wound around the core, the method being characterized in that said insulating material is compatible with said operating temperature and is put into place on said core without subsequent heating.
= CA 02575625 2013-11-27 In a first preferred implementation, said insulating material is extruded onto said core.
Preferably, said insulating material is a poly-ether-ether-ketone.
Advantageously, said insulating material is poly (oxy-1,4-phenylene-oxy-1,4-phenylene-carbony1-1,4-phenylene).
In a second preferred implementation, said insulating material is constituted by at least one tape placed on said core.
Preferably, the nature of the insulating material is glass fiber.
Preferably, the invention also provides an electricity transport conductor made by such a method, said conductor wires are wound to form at least one layer covering said core, itself covered in said insulating material.
Preferably, the conductor includes a plurality of composite cores, at least one of which is covered in a said layer of insulating material.
It may also comprise a plurality of composite cores contained in a common said layer of insulating material.
Said conductor wires may be wires of round shape, of trapezoidal shape, or of Z shape.
Said fibers are preferably made of carbon.
The invention is described below in greater detail with reference to figures that merely show preferred implementations of the invention.
Figures 1 to 6 are cross-section views of electricity transport conductors in accordance with the invention.
These figures show an electricity transport conductor, in particular for overhead power lines presenting an operating temperature that is greater than or equal to 200 C. The conductor comprises at least one composite central core 1 made up of fibers, preferably continuous filaments of carbon fibers, impregnated by a matrix of thermosetting resin, preferably epoxy resin, the core being covered in a 3a layer of insulating material 2, and by conductor wires of aluminum or aluminum alloy 3 that are wound around the core.
By using a pultrusion method, the continuous fibers are impregnated with resin, and then the resulting core is subjected to heat treatment with its temperature being raised continuously.
The invention relates to an electricity transport conductor for high voltage overhead lines.
The invention ,relates more particularly to a conductor comprising at least one composite central core made up of continuous fibers and impregnated by a matrix of thermosetting resin, and conductor wires of aluminum or aluminum alloy disposed around the core.
Such a conductor is described in patent document JP 03-129606.
In that prior art document, the composite core is constituted by organic or inorganic fibers, e.g. aramid, silicon carbide, or carbon fibers, impregnated by a synthetic resin, preferably an epoxy resin. That core may be coated in a polyimide resin or it may be taped in a polyimide film, forming an insulating layer. Conductor wires of aluminum are wound around such a core or a set of such cores in order to form an electricity transport conductor.
The function of the polyimide covering is to avoid problems of corrosion at the interface between the conductor wires and the core including carbon fibers.
Regardless of whether the polyimide covering is made by coating or by taping, it is necessary to pass the covered core through a drying oven after the covering has been put into place.
With conductors for overhead lines, there are three types of temperature to be taken into consideration:
= the maximum temperature acceptable under steady conditions;
= the maximum temperature acceptable during overloads of short, medium, or long duration; and = the maximum temperature acceptable during a short circuit.
It can be desired to make overhead line conductors that are designed in such a manner that the maximum acceptable temperature in all three of the above circumstances is greater than or equal to 200 C, which temperature is referred to below as the operating temperature.
In order to form a continuous insulating sheath of polyimide around the core, it is necessary to heat said taped or coated polyimide layer to a temperature greater than 300 C. Under such conditions, the insulating layer as formed in that way is compatible with a conductor having its operating temperature greater than or equal to 200 C.
Unfortunately, applying heat treatment at such a temperature greater than 300 C degrades the epoxy resin of the core, which begins to deteriorate at a temperature of about 250 C.
It can therefore be seen that fabrication in that way does not enable an electric cable to be obtained having an operating temperature that can be as high as 200 C or more.
According to the present invention, there is provided an electricity transport conductor, having an operating temperature greater than or equal to 200 C, said conductor comprising a plurality of composite central cores made of continuous fibers impregnated by a matrix of epoxy resin, wherein conductor wires of aluminum or aluminum alloy being wound directly around the composite central cores to form at least one layer covering said composite central cores and characterized in that each of said cores is covered in at least one extruded layer of insulating material.
Preferably, there is also provided a method of fabricating an electricity transport conductor, in particular for overhead power lines, having an operating temperature greater than or equal to 200 C and including at least one composite central core made of continuous fibers impregnated by a matrix of epoxy resin, the core being covered in at least one layer of insulating material, and conductor wires of aluminum or aluminum alloy being wound around the core, the method being characterized in that said insulating material is compatible with said operating temperature and is put into place on said core without subsequent heating.
= CA 02575625 2013-11-27 In a first preferred implementation, said insulating material is extruded onto said core.
Preferably, said insulating material is a poly-ether-ether-ketone.
Advantageously, said insulating material is poly (oxy-1,4-phenylene-oxy-1,4-phenylene-carbony1-1,4-phenylene).
In a second preferred implementation, said insulating material is constituted by at least one tape placed on said core.
Preferably, the nature of the insulating material is glass fiber.
Preferably, the invention also provides an electricity transport conductor made by such a method, said conductor wires are wound to form at least one layer covering said core, itself covered in said insulating material.
Preferably, the conductor includes a plurality of composite cores, at least one of which is covered in a said layer of insulating material.
It may also comprise a plurality of composite cores contained in a common said layer of insulating material.
Said conductor wires may be wires of round shape, of trapezoidal shape, or of Z shape.
Said fibers are preferably made of carbon.
The invention is described below in greater detail with reference to figures that merely show preferred implementations of the invention.
Figures 1 to 6 are cross-section views of electricity transport conductors in accordance with the invention.
These figures show an electricity transport conductor, in particular for overhead power lines presenting an operating temperature that is greater than or equal to 200 C. The conductor comprises at least one composite central core 1 made up of fibers, preferably continuous filaments of carbon fibers, impregnated by a matrix of thermosetting resin, preferably epoxy resin, the core being covered in a 3a layer of insulating material 2, and by conductor wires of aluminum or aluminum alloy 3 that are wound around the core.
By using a pultrusion method, the continuous fibers are impregnated with resin, and then the resulting core is subjected to heat treatment with its temperature being raised continuously.
Such a core providing mechanical reinforcement has the advantages of presenting specific weight that is low, and of accepting mechanical stresses that are high.
The core constituted by a plurality of continuous carbon fiber filaments that are assembled together and impregnated with epoxy resin is such that:
= its breaking stress is greater than or equal to 2.6 gigapascals (GPa);
= its breaking elongation is greater than 2%;
= its modulus of elasticity is greater than 90 GPa;
= its coefficient of linear expansion is less than 2x10-6/ C;
= its specific weight is less than 2 kilograms per cubic decimeter (kg/dm3);
= its carbon fiber content by weight is greater than 70%;
= after aging for 30 days at the operating temperature of 200 C, its breaking stress is greater than or equal to 2.6 GPa, and this applies under both of the following circumstances: core under a mechanical load of 25% of its initial breaking stress, and core under no mechanical load; and = after being wound through 180 on a maximum diameter of 120 times the diameter of the core and then subjected on three consecutive occasions to a mechanical load equal to 25% of its initial breaking stress, the core presents breaking stress greater than or equal to 2.6 GPa.
The number of composite cores used for a conductor is such that it passes an alternating bending test for demonstrating that the stresses present during stringing, i.e. while passing under mechanical tension through pulleys does not affect or degrade the performance of the conductor.
The conductor is tensioned to 15% of its nominal breaking load. A carriage is installed on the conductor, the carriage comprising three pulleys placed in a vertical plane and having their axes placed in a common horizontal plane. The spacing between the extreme pulleys is 3200 millimeters (mm) 600 mm.
The pulleys are of the same type as those used when 5 stringing conventional conductors on overhead lines (the groove bottoms are lined with neoprene):
Diameter of bottom of pulley groove Diameter of conductor (mm) (mm) 800 =38 1000 > 38 The carriage performs go-and-return movements at a horizontal speed lying in the range 0.5 meters per second (m/s) to 2 m/s over a distance lying in the range 50 meters (m) to 60 m. The acceleration and breaking are carried out without jolting.
The assembly comprising the conductor and the accessories must withstand at least 95% of the nominal breaking load of the conductor.
In Figure 1, a single core 1 is located centrally and is covered in a layer of insulating material 2.
Conductor wires 3 of aluminum or aluminum alloy, in this case wires of Z shape, are wound on the core in two layers.
In Figure 2, a single core 1 is located centrally and is covered in a layer of insulating material 2.
Conductor wires 3 of aluminum or aluminum alloy, in this case wires of trapezoid shape, are wound on the core in two layers.
In Figure 3, three cores 1A, 1B, and 1C are disposed centrally, each core being covered in a layer of insulating material 2A, 2B, 2C. Conductor wires 3 of aluminum or aluminum alloy, in this case of Z shape, are wound on these cores in three layers.
In Figure 4, three cores 1A, 1B, and 10 are disposed centrally and are covered in a single layer of insulating material 2. Conductor wires 3 of aluminum or aluminum alloy, in this case wires of trapezoid shape, are wound on these cores in two layers.
In Figure 5, three cores 1A, 1B, and 1C are disposed centrally and are covered firstly in respective layers of insulating material 2A, 2B, 2C, and secondly in a common layer of insulating material 2. Conductor wires 3 of aluminum or aluminum alloy, in this case of trapezoid shape, are wound on these cores in two layers.
In Figure 6, three cores 1A, 1B, and 1C are disposed centrally, each being covered in a respective layer of insulating material 2A, 2B, 2C. Conductor wires 3 of aluminum or aluminum alloy are wound on these cores in three layers, a first layer being made up of round wires 3A, a second layer of Z-shaped wires 3B, and a third layer of trapezoid-shaped wires 3C.
According to the invention, the insulating material of the layers 2 is compatible with the operating temperature being greater than or equal to 200 C and is put into place on the core 1 without subsequent heating.
In a first implementation, the insulating material is extruded onto the core 1 and is constituted by a poly-ether-ether-ketone.
Preferably, use is made of poly (oxy-1,4-phenylene-oxy-1,4-phenylene-carbonyl-1,4-phenylene), as sold under the name Victrex PEEK.
In a second implementation, the insulating material is constituted by at least one tape of glass fibers.
The core constituted by a plurality of continuous carbon fiber filaments that are assembled together and impregnated with epoxy resin is such that:
= its breaking stress is greater than or equal to 2.6 gigapascals (GPa);
= its breaking elongation is greater than 2%;
= its modulus of elasticity is greater than 90 GPa;
= its coefficient of linear expansion is less than 2x10-6/ C;
= its specific weight is less than 2 kilograms per cubic decimeter (kg/dm3);
= its carbon fiber content by weight is greater than 70%;
= after aging for 30 days at the operating temperature of 200 C, its breaking stress is greater than or equal to 2.6 GPa, and this applies under both of the following circumstances: core under a mechanical load of 25% of its initial breaking stress, and core under no mechanical load; and = after being wound through 180 on a maximum diameter of 120 times the diameter of the core and then subjected on three consecutive occasions to a mechanical load equal to 25% of its initial breaking stress, the core presents breaking stress greater than or equal to 2.6 GPa.
The number of composite cores used for a conductor is such that it passes an alternating bending test for demonstrating that the stresses present during stringing, i.e. while passing under mechanical tension through pulleys does not affect or degrade the performance of the conductor.
The conductor is tensioned to 15% of its nominal breaking load. A carriage is installed on the conductor, the carriage comprising three pulleys placed in a vertical plane and having their axes placed in a common horizontal plane. The spacing between the extreme pulleys is 3200 millimeters (mm) 600 mm.
The pulleys are of the same type as those used when 5 stringing conventional conductors on overhead lines (the groove bottoms are lined with neoprene):
Diameter of bottom of pulley groove Diameter of conductor (mm) (mm) 800 =38 1000 > 38 The carriage performs go-and-return movements at a horizontal speed lying in the range 0.5 meters per second (m/s) to 2 m/s over a distance lying in the range 50 meters (m) to 60 m. The acceleration and breaking are carried out without jolting.
The assembly comprising the conductor and the accessories must withstand at least 95% of the nominal breaking load of the conductor.
In Figure 1, a single core 1 is located centrally and is covered in a layer of insulating material 2.
Conductor wires 3 of aluminum or aluminum alloy, in this case wires of Z shape, are wound on the core in two layers.
In Figure 2, a single core 1 is located centrally and is covered in a layer of insulating material 2.
Conductor wires 3 of aluminum or aluminum alloy, in this case wires of trapezoid shape, are wound on the core in two layers.
In Figure 3, three cores 1A, 1B, and 1C are disposed centrally, each core being covered in a layer of insulating material 2A, 2B, 2C. Conductor wires 3 of aluminum or aluminum alloy, in this case of Z shape, are wound on these cores in three layers.
In Figure 4, three cores 1A, 1B, and 10 are disposed centrally and are covered in a single layer of insulating material 2. Conductor wires 3 of aluminum or aluminum alloy, in this case wires of trapezoid shape, are wound on these cores in two layers.
In Figure 5, three cores 1A, 1B, and 1C are disposed centrally and are covered firstly in respective layers of insulating material 2A, 2B, 2C, and secondly in a common layer of insulating material 2. Conductor wires 3 of aluminum or aluminum alloy, in this case of trapezoid shape, are wound on these cores in two layers.
In Figure 6, three cores 1A, 1B, and 1C are disposed centrally, each being covered in a respective layer of insulating material 2A, 2B, 2C. Conductor wires 3 of aluminum or aluminum alloy are wound on these cores in three layers, a first layer being made up of round wires 3A, a second layer of Z-shaped wires 3B, and a third layer of trapezoid-shaped wires 3C.
According to the invention, the insulating material of the layers 2 is compatible with the operating temperature being greater than or equal to 200 C and is put into place on the core 1 without subsequent heating.
In a first implementation, the insulating material is extruded onto the core 1 and is constituted by a poly-ether-ether-ketone.
Preferably, use is made of poly (oxy-1,4-phenylene-oxy-1,4-phenylene-carbonyl-1,4-phenylene), as sold under the name Victrex PEEK.
In a second implementation, the insulating material is constituted by at least one tape of glass fibers.
Claims (5)
1. An electricity transport conductor, having an operating temperature greater than or equal to 200°C, said conductor comprising a plurality of composite central cores made of continuous fibers impregnated by a matrix of epoxy resin, wherein conductor wires of aluminum or aluminum alloy being wound directly around the composite central cores to form at least one layer covering said composite central cores and characterized in that each of said cores is covered in at least one extruded layer of insulating material.
2. The electricity transport conductor according to claim 1, characterized in that said insulating material is a poly-ether-ether-ketone.
3. The electricity transport conductor according to claim 2, characterized in that said insulating material is poly (oxy-1,4-phenylene-oxy-1,4-phenylene-carbonyl-1,4-phenylene).
4. The electricity transport conductor according to any one of claims 1 to 3, characterized in that said conductor wires (3) are wires of round shape, of trapezoid shape, or of Z shape.
5. The electricity transport conductor according to any one of claims 1 to 4, characterized in that said fibers are of carbon.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0650354A FR2896911B1 (en) | 2006-02-01 | 2006-02-01 | ELECTRICAL TRANSPORT CONDUCTOR FOR AERIAL LINE |
| FR0650354 | 2006-02-01 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2575625A1 CA2575625A1 (en) | 2007-08-01 |
| CA2575625C true CA2575625C (en) | 2015-04-07 |
Family
ID=37003388
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA 2575625 Expired - Fee Related CA2575625C (en) | 2006-02-01 | 2007-01-25 | An electricity transport conductor for overhead lines |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20070193767A1 (en) |
| EP (1) | EP1816654B1 (en) |
| KR (1) | KR20070079320A (en) |
| AU (1) | AU2007200369B2 (en) |
| BR (1) | BRPI0700216A (en) |
| CA (1) | CA2575625C (en) |
| FR (1) | FR2896911B1 (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8969728B2 (en) | 2009-08-18 | 2015-03-03 | Halliburton Energy Services, Inc. | Smooth wireline |
| WO2011143541A2 (en) * | 2010-05-14 | 2011-11-17 | Zoltek Companies, Inc. | Carbon fiber composite structural rod and method of manufacture |
| CA2800839A1 (en) * | 2010-07-11 | 2012-01-19 | Halliburton Energy Services, Inc. | Downhole cables for well operations |
| HUE033251T2 (en) | 2011-04-12 | 2017-11-28 | Southwire Co Llc | Electrical transmission cables with composite cores |
| TW201308362A (en) | 2011-04-12 | 2013-02-16 | Ticona Llc | Composite core for electrical transmission cables |
| EP2697040B1 (en) | 2011-04-12 | 2016-08-17 | Ticona LLC | Die and method for impregnating fiber rovings |
| JP6045566B2 (en) | 2011-04-12 | 2016-12-14 | ティコナ・エルエルシー | Die impregnation section and method for impregnating fiber roving |
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| CA2831358C (en) | 2011-04-12 | 2019-04-02 | Ticona Llc | Continuous fiber reinforced thermoplastic rods and pultrusion method for its manufacture |
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| CA2775445C (en) | 2011-04-29 | 2019-04-09 | Ticona Llc | Die and method for impregnating fiber rovings |
| CN104053530B (en) | 2011-04-29 | 2016-10-19 | 提克纳有限责任公司 | For impregnating the mould with flowing diffusion cast path and the method for fiber roving |
| US10336016B2 (en) | 2011-07-22 | 2019-07-02 | Ticona Llc | Extruder and method for producing high fiber density resin structures |
| CN102354566A (en) * | 2011-09-19 | 2012-02-15 | 沈阳电业局电缆厂 | Fiber insulation core overhead conducting wire |
| WO2013102913A2 (en) * | 2011-10-19 | 2013-07-11 | Sterlite Technologies Ltd. | Electrical power conductor |
| US9409355B2 (en) | 2011-12-09 | 2016-08-09 | Ticona Llc | System and method for impregnating fiber rovings |
| US9283708B2 (en) | 2011-12-09 | 2016-03-15 | Ticona Llc | Impregnation section for impregnating fiber rovings |
| US9321073B2 (en) | 2011-12-09 | 2016-04-26 | Ticona Llc | Impregnation section of die for impregnating fiber rovings |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3980808A (en) * | 1974-09-19 | 1976-09-14 | The Furukawa Electric Co., Ltd. | Electric cable |
| JPH03129606A (en) * | 1989-07-27 | 1991-06-03 | Hitachi Cable Ltd | Aerial power cable |
| DE60136116D1 (en) * | 2000-02-08 | 2008-11-27 | Brandt Goldsworthy & Associate | Electric reinforced transmission network conductor |
| US20040182597A1 (en) * | 2003-03-20 | 2004-09-23 | Smith Jack B. | Carbon-core transmission cable |
| US7093416B2 (en) * | 2004-06-17 | 2006-08-22 | 3M Innovative Properties Company | Cable and method of making the same |
| US7399339B2 (en) * | 2005-06-15 | 2008-07-15 | Gas Technology Institute | Polyoxometalate material for gaseous stream purification at high temperature |
-
2006
- 2006-02-01 FR FR0650354A patent/FR2896911B1/en not_active Expired - Fee Related
-
2007
- 2007-01-25 CA CA 2575625 patent/CA2575625C/en not_active Expired - Fee Related
- 2007-01-26 US US11/698,795 patent/US20070193767A1/en not_active Abandoned
- 2007-01-29 AU AU2007200369A patent/AU2007200369B2/en not_active Ceased
- 2007-01-31 KR KR1020070010295A patent/KR20070079320A/en not_active Application Discontinuation
- 2007-01-31 BR BRPI0700216-5A patent/BRPI0700216A/en not_active IP Right Cessation
- 2007-01-31 EP EP20070300754 patent/EP1816654B1/en not_active Not-in-force
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|---|---|
| AU2007200369A1 (en) | 2007-08-16 |
| KR20070079320A (en) | 2007-08-06 |
| FR2896911A1 (en) | 2007-08-03 |
| US20070193767A1 (en) | 2007-08-23 |
| BRPI0700216A (en) | 2007-11-06 |
| EP1816654B1 (en) | 2015-04-29 |
| CA2575625A1 (en) | 2007-08-01 |
| EP1816654A2 (en) | 2007-08-08 |
| EP1816654A3 (en) | 2014-04-30 |
| AU2007200369B2 (en) | 2013-01-24 |
| FR2896911B1 (en) | 2008-03-21 |
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| EEER | Examination request | ||
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